US4811309A - Microphone probe for acoustic measurement in turbulent flow - Google Patents
Microphone probe for acoustic measurement in turbulent flow Download PDFInfo
- Publication number
- US4811309A US4811309A US07/094,753 US9475387A US4811309A US 4811309 A US4811309 A US 4811309A US 9475387 A US9475387 A US 9475387A US 4811309 A US4811309 A US 4811309A
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- tube
- probe
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- 239000000523 sample Substances 0.000 title claims abstract description 62
- 238000005259 measurement Methods 0.000 title claims abstract description 8
- 239000000463 material Substances 0.000 claims abstract description 51
- 238000011144 upstream manufacturing Methods 0.000 claims abstract description 6
- 239000010410 layer Substances 0.000 claims description 40
- 239000002184 metal Substances 0.000 claims description 8
- 230000001902 propagating effect Effects 0.000 claims description 2
- 230000000644 propagated effect Effects 0.000 claims 1
- 239000011241 protective layer Substances 0.000 claims 1
- 238000010276 construction Methods 0.000 description 6
- 238000012935 Averaging Methods 0.000 description 4
- 239000011152 fibreglass Substances 0.000 description 4
- 239000000853 adhesive Substances 0.000 description 2
- 230000001070 adhesive effect Effects 0.000 description 2
- 230000001681 protective effect Effects 0.000 description 2
- 239000012814 acoustic material Substances 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- 230000004323 axial length Effects 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 239000000835 fiber Substances 0.000 description 1
- 239000002657 fibrous material Substances 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000002356 single layer Substances 0.000 description 1
- 238000004804 winding Methods 0.000 description 1
Images
Classifications
-
- G—PHYSICS
- G10—MUSICAL INSTRUMENTS; ACOUSTICS
- G10K—SOUND-PRODUCING DEVICES; METHODS OR DEVICES FOR PROTECTING AGAINST, OR FOR DAMPING, NOISE OR OTHER ACOUSTIC WAVES IN GENERAL; ACOUSTICS NOT OTHERWISE PROVIDED FOR
- G10K11/00—Methods or devices for transmitting, conducting or directing sound in general; Methods or devices for protecting against, or for damping, noise or other acoustic waves in general
- G10K11/004—Mounting transducers, e.g. provided with mechanical moving or orienting device
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04R—LOUDSPEAKERS, MICROPHONES, GRAMOPHONE PICK-UPS OR LIKE ACOUSTIC ELECTROMECHANICAL TRANSDUCERS; DEAF-AID SETS; PUBLIC ADDRESS SYSTEMS
- H04R1/00—Details of transducers, loudspeakers or microphones
- H04R1/08—Mouthpieces; Microphones; Attachments therefor
- H04R1/083—Special constructions of mouthpieces
- H04R1/086—Protective screens, e.g. all weather or wind screens
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04R—LOUDSPEAKERS, MICROPHONES, GRAMOPHONE PICK-UPS OR LIKE ACOUSTIC ELECTROMECHANICAL TRANSDUCERS; DEAF-AID SETS; PUBLIC ADDRESS SYSTEMS
- H04R3/00—Circuits for transducers, loudspeakers or microphones
- H04R3/005—Circuits for transducers, loudspeakers or microphones for combining the signals of two or more microphones
Definitions
- Sound energy emitted by sound sources is often measured through use of a microphone but the measurement is often complicated because of the presence of flow noise.
- Flow noise can be generated by two sources. First, there is self-noise caused by the presence of the microphone unit itself. Microphone nose cones and wind screens can act to reduce this self-noise. Second, there is flow noise associated with the turbulent pressure fluctuations caused by the fan. Probe tubes have been proposed in an attempt to desensitize the microphones to turbulent flow pressure fluctuations. In general, the microphone probes, as used in the past, have consisted of an elongated tube having a tapered end facing upstream of the direction of sound propagation and containing a microphone in the opposite end. The tube includes a plurality of small spaced openings, or alternately, an elongated slit, which is covered with an acoustically resistive material, such as cloth or felt.
- Screens of this type are designed to distinguish between turbulent pressure fluctuations, which have a low propagation velocity, and sound pressure fluctuations, which have a much higher propagation velocity.
- Pressure fluctuations at locations on the tube cause pressure waves to propagate inside of the tube with the propagation velocity being nearly equal to the speed of sound. If the pressure fluctuations are sound waves, the pressure waves from all locations will add constructively and create a high sound pressure at the microphone because the propagation velocity of the sound inside and outside of the tube is nearly the same.
- the invention is directed to an improved microphone probe for measuring acoustical energy in turbulent flow.
- the probe comprises an elongated tube having a closed end facing upstream in the direction of sound propagation and having a microphone located in the downstream end of the tube.
- the tube can be formed with an elongated slit.
- an acoustically resistive material is stretched across the holes and clamped to the tube.
- the side edges of the material are connected to a pair of rigid bars and the bars are drawn together at a location opposite the holes by adjustable fasteners, such as bolts, to stretch the material over the holes and thereby provide uniform acoustical resistance for the portions of the material enclosing the holes.
- adjustable fasteners such as bolts
- the acoustical resistive material can be either woven or unwoven fibrous material, such as fiber glass or felt, and can also include a protective outer metal screen.
- the side edges of the acoustically resistive material are connected to a pair of elongated rods and the rods are clamped together by spring clips to stretch the material across the holes.
- the side edges of the material can be connected to the rods through resilient C-shaped clamps, and spring clips are then employed to clamp the C-clamps together to stretch the material across the holes.
- the invention enables the acoustically resistive material to be uniformly stretched across the series of holes to provide uniform acoustical resistance throughout the length of the tube, and the material can be readily adjusted in tautness to vary the flow resistance, as desired.
- the clamping mechanism as used in the invention, enables multiple layers of acoustical media to be utilized, and the mechanism can be readily assembled and disassembled with the tube for service or replacement of the acoustical media.
- a plurality of microphone probes can be disposed in parallel relation in the duct with the closed ends of the probes facing the source of sound energy.
- the signal generated by the microphone of each probe is transmitted to a summing amplifier which produces a summed output signal.
- a plurality of probes that are disposed in parallel relation in the sound duct are joined to a single microphone which generates an output signal.
- the turbulent pressure fluctuations are randomly distributed in the sound duct and the use of a plurality of probes provides more precise spatial averaging of the random pressure fluctuations.
- FIG. 1 is a side elevation of the microphone measuring probe of the invention
- FIG. 2 is an enlarged fragmentary longitudinal section of the end of the probe
- FIG. 3 is a section taken along line 3--3 of FIG. 2;
- FIG. 4 is an enlarged transfer section showing the acoustic media attached to clamping strips
- FIG. 5 is a view similar to FIG. 4 showing a modified form of the invention in which the acoustic media is attached to the clamping strips through use of an adhesive;
- FIG. 6 is a view similar to FIG. 3 and shows a modified form of the invention in which the ends of the acoustic media are attached to the tube through use of a spring clip;
- FIG. 7 is a view similar to FIG. 6 showing another form of the invention in which the ends of the acoustic media are attached to longitudinal rods through use of clamps and spring clips connect the clamps together;
- FIG. 8 is a view similar to FIG. 7 showing a further modified form of the invention in which the clamps are welded to the tube;
- FIG. 9 is a schematic representation of a system utilizing a pair of microphone probes which are connected to a summing amplifier.
- FIG. 10 is a schematic representation of a system using a pair of probes that are joined to a single microphone.
- FIG. 1 illustrates a microphone probe to be used for acoustical measurement in turbulent flow.
- Probe 1 includes an elongated metal tube 2 having a bent outer end carrying a mounting plate 3 that is adapted to be mounted on a duct 4 or other conduit through which sound is propagating. While the drawings illustrate the probe 1 used in association with a duct, it is contemplated that the probe can be utilized in any fluid flow path to measure the sound energy.
- a conventional microphone 5 is located within the outer bent end of tube 2 and the end of the tube can be connected through coupling 6 to a conduit which contains the electrical leads connected to microphone 5.
- the inner end of tube 2 faces upstream in the direction of sound propagation in duct 4 and is closed off by a plug 7 of acoustical media, such as felt, that is located within a sleeve 8 attached to the end of tube 2.
- a plug 7 of acoustical media such as felt
- tube 2 Spaced along the length of tube 2 are a plurality of holes or openings 9, which extend substantially the full length of the straight inner section of tube 2. While the drawings illustrate the use of openings 9, it is contemplated that as an alternate construction, tube 2 can contain an elongated continuous slit.
- a strip 10 of acoustically resistive material such as fiber glass
- a second layer 11 of acoustically resistive material such as felt
- an outer protective metal screen 12 can be positioned around the layer 11 and is generally co-extensive in circumferential width with layer 10.
- Both the layer 11 and screen 12 are provided with reversely bent ends, 13 and 14 respectively, which are secured around metal strips 15.
- Layers 10 and 11, as well as screen 12 and strips 15, all have a comparable axial length.
- strips 15 are located generally diametrically opposite the openings 9, and the strips are drawn together to clamp and stretch the layers 10 and 11 across the openings 9.
- the clamping is accomplished through use of a plurality of bolts 16, which are spaced along the length of tube 2 and extend through aligned openings in strips 15 as well as through layer 11 and screen 12.
- the threaded ends of bolts 16 receive nuts 17. By threading down the nuts 17, the acoustical media will be stretched across openings 9.
- the flow resistivity of the acoustic media is dependent on its density and the fiber diameter.
- the felt layer 11 has sufficient strength and integrity so that it can be stretched without tearing or rupturing.
- FIG. 4 illustrates the pre-assembly of the acoustical layers to strips 15 prior to assembly with tube 2.
- the ends 18 of layer 11 and screen 12 can be connected to the main body of these layers by stitching, or mechanical fasteners, so that the side edges of the media layers are firmly connected around strips 15.
- FIG. 5 is a view similar to FIG. 4 showing an alternate method of connecting the acoustical resistive layer 11 to the metal strips 15.
- the side edges of the layer 11 are bent or rolled around the strips 15 and the side edges are connected to the strips by a layer of an adhesive 19.
- the acoustical layer 11 as shown in FIG. 5 can be wrapped over the layer 10 on tube 2 and clamped to the tube in the manner illustrated in FIGS. 1-3.
- FIG. 6 illustrates a modified form of the invention in which the openings 9 in tube 2 are enclosed by a strip 20 of acoustically resistive material, such as fiber glass, similar to the strip 10 of the first embodiment.
- a second layer 21 of acoustically resistive material, such as felt, is wrapped over strip 20 and the side edges of layer 21 are attached around metal rods 22 by stitching or mechanical fasteners.
- Resilient spring clips 23 are employed to clamp rods 22 together, and as shown in FIG. 6, the side flanges 24 of the clips 23 engage the rods and the resilient nature of the clips acts to draw the rods together to stretch the acoustical media over the openings 9.
- a group of spring clips 23 can be utilized which are spaced along the length of the rods 21, or alternately, single spring clip having a length approximately the same as rods 21 can be employed.
- FIG. 7 shows a further modified form of the invention in which a strip 25 of acoustic media, such as fiber glass, is positioned over the row of holes 9 and is covered by a layer of acoustic media 26, such as felt.
- a layer of acoustic media 26 such as felt.
- the longitudinal side edges of the felt layer 26 are clamped to longitudinal rods 27 by resilient C-clamps 28 so that the edges of the felt are firmly secured to the rods.
- Clips 29, similar in construction and function to clips 23, are utilized to clamp the rods 27 together to thereby stretch the acoustic media across the holes 9.
- FIG. 8 shows a further modified form of the invention which is similar to that described in FIG. 7 except that the inner ends of the C-clamps 28 are permanently affixed as by welds 30 to the outer surface of tube 2. As previously described, the clamps 28 serve rods 27 and the spring clips 29 act to draw the rods together to stretch the acoustic media over the holes 9.
- the invention provides an improved microphone probe for acoustical measurement in turbulent flow in which the acoustic media is stretched in a taut and uniform condition across the openings in the probe.
- the invention also includes a mechanism for adjusting the tension on the acoustic media to thereby vary the acoustical resistance of the material, as desired.
- the mechanism of the invention can be employed to attach a single or multiple layers of acoustic media to the probe.
- the turbulent pressure fluctuations are randomly distributed in duct 4, and to provide a more accurate spatial averaging of the fluctuations, two or more probes 31 can be utilized, as shown in FIG. 9.
- the probes 31, which can be of similar construction to the probes previously described, are mounted in spaced parallel relation in duct 4, preferably at diametrically opposite locations.
- the probes can be offset longitudinally, but the offset distance should be substantially less than the wave length of the sound energy.
- the microphone 32 of each probe 31 is connected by leads 33 to a summing amplifier 34 which generates a summed output signal.
- the use of the plurality of probes provides more precise spatial averaging of the random turbulent pressure fluctuations in duct 4.
- FIG. 10 illustrates a further modified form of the invention employing a plurality of probes.
- a pair of probes 35 similar in construction to the probes previously described, are positioned in spaced parallel relation in duct 4.
- the corresponding ends of probes 35 facing away from the source of sound energy, are bent laterally, as indicated by 36, and joined together at an extension 37.
- a single microphone 38 is located in extension 36.
- the system of FIG. 10 using a plurality of probes 35, provides a more accurate averaging of the randomly distributed turbulent pressure fluctuations in duct 4.
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- Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- Acoustics & Sound (AREA)
- Signal Processing (AREA)
- Health & Medical Sciences (AREA)
- General Health & Medical Sciences (AREA)
- Otolaryngology (AREA)
- Multimedia (AREA)
- Measurement Of Mechanical Vibrations Or Ultrasonic Waves (AREA)
Abstract
Description
Claims (24)
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US07/094,753 US4811309A (en) | 1987-09-04 | 1987-09-04 | Microphone probe for acoustic measurement in turbulent flow |
CA000576192A CA1321637C (en) | 1987-09-04 | 1988-08-31 | Microphone probe for acoustic measurement in turbulent flow |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US07/094,753 US4811309A (en) | 1987-09-04 | 1987-09-04 | Microphone probe for acoustic measurement in turbulent flow |
Publications (1)
Publication Number | Publication Date |
---|---|
US4811309A true US4811309A (en) | 1989-03-07 |
Family
ID=22246977
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US07/094,753 Expired - Lifetime US4811309A (en) | 1987-09-04 | 1987-09-04 | Microphone probe for acoustic measurement in turbulent flow |
Country Status (2)
Country | Link |
---|---|
US (1) | US4811309A (en) |
CA (1) | CA1321637C (en) |
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4903249A (en) * | 1988-03-24 | 1990-02-20 | Nelson Industries | Rigid foraminous microphone probe for acoustic measurement in turbulent flow |
US5224168A (en) * | 1991-05-08 | 1993-06-29 | Sri International | Method and apparatus for the active reduction of compression waves |
US5418873A (en) * | 1993-09-09 | 1995-05-23 | Digisonix, Inc. | Active acoustic attenuation system with indirect error sensing |
US5477506A (en) * | 1993-11-10 | 1995-12-19 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | In-flow acoustic sensor |
US5660255A (en) * | 1994-04-04 | 1997-08-26 | Applied Power, Inc. | Stiff actuator active vibration isolation system |
US5680337A (en) * | 1994-05-23 | 1997-10-21 | Digisonix, Inc. | Coherence optimized active adaptive control system |
US20060283660A1 (en) * | 2005-06-15 | 2006-12-21 | Siemens Westinghouse Power Corporation | Acoustic termination for a pressure monitoring system |
US20070214864A1 (en) * | 2006-02-23 | 2007-09-20 | Asylum Research Corporation | Active Damping of High Speed Scanning Probe Microscope Components |
US9383388B2 (en) | 2014-04-21 | 2016-07-05 | Oxford Instruments Asylum Research, Inc | Automated atomic force microscope and the operation thereof |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3444955A (en) * | 1964-08-01 | 1969-05-20 | Sennheiser Electronic | Directional microphone with substantially frequency-independent directional characteristics |
US4421957A (en) * | 1981-06-15 | 1983-12-20 | Bell Telephone Laboratories, Incorporated | End-fire microphone and loudspeaker structures |
US4703506A (en) * | 1985-07-23 | 1987-10-27 | Victor Company Of Japan, Ltd. | Directional microphone apparatus |
-
1987
- 1987-09-04 US US07/094,753 patent/US4811309A/en not_active Expired - Lifetime
-
1988
- 1988-08-31 CA CA000576192A patent/CA1321637C/en not_active Expired - Fee Related
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3444955A (en) * | 1964-08-01 | 1969-05-20 | Sennheiser Electronic | Directional microphone with substantially frequency-independent directional characteristics |
US4421957A (en) * | 1981-06-15 | 1983-12-20 | Bell Telephone Laboratories, Incorporated | End-fire microphone and loudspeaker structures |
US4703506A (en) * | 1985-07-23 | 1987-10-27 | Victor Company Of Japan, Ltd. | Directional microphone apparatus |
Non-Patent Citations (14)
Title |
---|
"Measuring Microphones, Studio Microphones, Hydrophones and Accessory Equipment" Group 3 UA0436. |
"Noise & Vibration Control", Beranek, McGraw-Hill Book Company, 1971. |
J. Acoust, Soc. Am, "Tubular Windscreen Design for Microphones for In-Duct Fan Sound Power Measurements", Wang et al., vol. 55, No. 3, Mar. 1974. |
J. Acoust, Soc. Am, Tubular Windscreen Design for Microphones for In Duct Fan Sound Power Measurements , Wang et al., vol. 55, No. 3, Mar. 1974. * |
Journal of Sound and Vibration "The Flow Noise Level at Microphones in Flow Ducts" Neiss et al., 1979, 63(4), 561-579. |
Journal of Sound and Vibration "Theoretical and Experimental Investigations of Microphone Probes for Sound Measurements in Turbulent Flow" 1975, vol. 39(3), 371-400. |
Journal of Sound and Vibration The Flow Noise Level at Microphones in Flow Ducts Neiss et al., 1979, 63(4), 561 579. * |
Journal of Sound and Vibration Theoretical and Experimental Investigations of Microphone Probes for Sound Measurements in Turbulent Flow 1975, vol. 39(3), 371 400. * |
Journal of Sound and Vibration, "Microphone Screens for Acoustic Measurement in Turbeltn Flows", Shepherd, 1986, Co. 111(1), 153-165. |
Journal of Sound and Vibration, Microphone Screens for Acoustic Measurement in Turbeltn Flows , Shepherd, 1986, Co. 111(1), 153 165. * |
Measuring Microphones, Studio Microphones, Hydrophones and Accessory Equipment Group 3 UA0436. * |
Noise & Vibration Control , Beranek, McGraw Hill Book Company, 1971. * |
The American Society of Mechanical Engineers, "Active Attenuation in Flow Ducts: Assessmen of Prospective Applications" Shephard et al., Dec. 1986. |
The American Society of Mechanical Engineers, Active Attenuation in Flow Ducts: Assessmen of Prospective Applications Shephard et al., Dec. 1986. * |
Cited By (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4903249A (en) * | 1988-03-24 | 1990-02-20 | Nelson Industries | Rigid foraminous microphone probe for acoustic measurement in turbulent flow |
US5224168A (en) * | 1991-05-08 | 1993-06-29 | Sri International | Method and apparatus for the active reduction of compression waves |
US5363451A (en) * | 1991-05-08 | 1994-11-08 | Sri International | Method and apparatus for the active reduction of compression waves |
US5418873A (en) * | 1993-09-09 | 1995-05-23 | Digisonix, Inc. | Active acoustic attenuation system with indirect error sensing |
US5477506A (en) * | 1993-11-10 | 1995-12-19 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | In-flow acoustic sensor |
US5660255A (en) * | 1994-04-04 | 1997-08-26 | Applied Power, Inc. | Stiff actuator active vibration isolation system |
US5680337A (en) * | 1994-05-23 | 1997-10-21 | Digisonix, Inc. | Coherence optimized active adaptive control system |
US20060283660A1 (en) * | 2005-06-15 | 2006-12-21 | Siemens Westinghouse Power Corporation | Acoustic termination for a pressure monitoring system |
US20070214864A1 (en) * | 2006-02-23 | 2007-09-20 | Asylum Research Corporation | Active Damping of High Speed Scanning Probe Microscope Components |
US8302456B2 (en) | 2006-02-23 | 2012-11-06 | Asylum Research Corporation | Active damping of high speed scanning probe microscope components |
US8763475B2 (en) | 2006-02-23 | 2014-07-01 | Oxford Instruments Asylum Research Corporation | Active damping of high speed scanning probe microscope components |
US9383388B2 (en) | 2014-04-21 | 2016-07-05 | Oxford Instruments Asylum Research, Inc | Automated atomic force microscope and the operation thereof |
US9921242B2 (en) | 2014-04-21 | 2018-03-20 | Oxford Instruments Asylum Research Inc | Automated atomic force microscope and the operation thereof |
Also Published As
Publication number | Publication date |
---|---|
CA1321637C (en) | 1993-08-24 |
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